An adaptive fuzzy control scheme with application in flexible spacecraft control

Author

Bahita, Mohamed ; Belarbi, Khaled

Author_Institution

Fac. of Chem. Eng., Univ. of Constantine 3, Constantine, Algeria

fYear

2014

fDate

9-12 Sept. 2014

Firstpage

25

Lastpage

30

Abstract

We introduce a direct fuzzy adaptive control for the large angle rotational movement and vibration suppression of a flexible spacecraft. A Takagi Sugeno inference system is used to approximate a feedback linearization control law. The adaptation mechanism is based on estimate of the error between the ideal unknown control signal and the actual control signal using a Mamdani fuzzy inference system. Simulation results show precise trajectory control and vibration suppression of the flexible spacecraft.

Keywords

adaptive control; fuzzy control; space vehicles; trajectory control; vibration control; Mamdani fuzzy inference system; Takagi Sugeno inference system; adaptation mechanism; direct fuzzy adaptive control; feedback linearization control law; flexible spacecraft control; large angle rotational movement; trajectory control; vibration suppression; Adaptation models; Adaptive control; Approximation methods; Computational modeling; Fuzzy logic; Space vehicles; Vibrations; Adaptive control; Fuzzy inference systems; flexible spacecraft;

fLanguage

English

Publisher

ieee

Conference_Titel

SICE Annual Conference (SICE), 2014 Proceedings of the

Conference_Location

Sapporo

Type

conf

DOI

10.1109/SICE.2014.6935179

Filename

6935179